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时间:2011-04-04 10:04来源:蓝天飞行翻译 作者:航空
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 57-30-01
 ALL  ú ú B01 Page 201 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 D. Procedure
 S 212-020-B00
 (1)  To help you find the applicable leading edge panel, see AMM 12-31-61/201.
 S 022-022-B00
 CAUTION: WHEN REMOVING PANEL FASTENERS, MAKE SURE THAT THE DRIVER BIT IS
_______ IN LINE WITH A FASTENER. THIS WILL PREVENT DRIVER BIT WOBBLE WHICH CAN CAUSE DAMAGE TO THE FASTENER RECESSES AND THREADS.
 (2) The following can help remove the bolts from the access panels:
 (a)  
A leverage adapter, B20004-21,

 (b)  
A removal anti cam-out ribbed (ACR) bit,


 NOTE: The bit should have a hardness of 56-58 RC.
____
 NOTE: A combination removal/installation ACR bit is not
____
 recommended.

 CAUTION: ONLY APPLY FASTENER REMOVAL COMPOUND DIRECTLY TO THE BIT
_______ IF NEEDED. CLEAN THE BIT AFTER EACH USE. DO NOT APPLY FASTENER REMOVAL COMPOUND TO THE FASTENER RECESSES, HOLES, OR THREADS. THIS CAN CAUSE DAMAGE TO THE FASTENERS.
 (c)  Apply a fastener removal compound on the driver bit if a fastener is difficult to remove.
 TASK 57-30-01-022-015-B00
 3. Installation of Difficult Fasteners
 A. Equipment
 (1)  Access Panel Leverage Adapter, B20004-21
 B. Consumable Materials
 (1)  Compound - Anti-seize, BMS 3-28
 C. References
 (1)  
12-31-61/201 Wing Lower Surface Access Doors and Panels

 (2)  
20-50-11/201 Standard Torque Values


 D. Access
 (1)  Location Zones
 300 Left Wing
 400 Right Wing

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 57-30-01
 ALL  ú ú B01 Page 202 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  Access Panels
 6212L/6512R Slat Access Panel
 6213L/6513R Slat Access Panel
 6214L/6514R Slat Access Panel
 6215L/6515R Slat Access Panel
 6217L/6517R Slat Access Panel
 6218L/6518R Slat Access Panel
 6219L/6519R Slat Access Panel
 6220L/6520R Slat Access Panel
 6221L/6521R Slat Access Panel
 6222L/6522R Slat Access Panel
 6223L/6523R Slat Access Panel
 6224L/6524R Slat Access Panel
 6225L/6525R Slat Access Panel
 6226L/6526R Slat Access Panel
 6227L/6527R Slat Access Panel
 6228L/6528R Slat Access Panel
 6229L/6529R Slat Access Panel
 6230L/6530R Slat Access Panel
 6231L/6531R Slat Access Panel
 6232L/6532R Slat Access Panel
 6233L/6533R Slat Access Panel
 6234L/6534R Slat Access Panel
 6241L/6541R Slat Access Panel

 E. Procedure
 S 212-018-B00
 (1)  To help you find the applicable leading edge panel, see AMM 12-31-61/201.
 S 422-017-B00
 CAUTION: WHEN INSTALLING FASTENERS, MAKE SURE THAT THE DRIVER BIT IS IN
_______ LINE WITH A FASTENER. THIS WILL PREVENT DRIVER BIT WOBBLE WHICH CAN CAUSE DAMAGE TO THE FASTENER RECESSES AND THREADS.
 (2)  The following can help install the bolts:
 NOTE:  These suggestions are to make sure that the bolts can be removed freely later and are not damaged when you install them.
 (a)  Use an access panel leverage adapter, B20004-21 to install the bolts.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 57-30-01
 ALL  ú ú B01 Page 203 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (b)  
Make sure that the fasteners have correct grip length, undamaged threads, and undamaged recesses.

 NOTE:  If any fasteners need to be replaced, it is recommended that K-coated titanium bolts with cadmium plated Cres nut-plates be installed where applicable.

 (c)  
Remove any excess paint or debris on fastener recesses.
 
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